Solution of the transonic airfoil problem through parametric differentiation.
LANDAHL, M. T. /MASSACHUSETTS INST. OF TECH., CAMBRIDGE, MASS./., RUBBERT, P. E. /BOEING CO., COMMERCIAL AIRPLANE DIV., RENTON, WASH./
AIAA Journal ; 5 , 3 ; 470-479
1967-01-01
10 pages
Article (Journal)
Electronic Resource
English
NTRS | 1979
|AIAA | 1971
|NTRS | 1984
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